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HAL Id: jpa-00210055

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Submitted on 1 Jan 1985

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Mode interaction in a spectrum of weakly unstable plasma waves

M. Trocheris

To cite this version:

M. Trocheris. Mode interaction in a spectrum of weakly unstable plasma waves. Journal de Physique,

1985, 46 (7), pp.1123-1135. �10.1051/jphys:019850046070112300�. �jpa-00210055�

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Mode interaction in a spectrum of weakly unstable plasma waves

M. Trocheris

Association EURATOM-CEA

sur

la fusion, Département de Recherches sur la Fusion Contrôlée, Centre d’Etudes Nucléaires, Boîte Postale n° 6, 92260 Fontenay-aux-Roses, France

(Reçu le 27 novembre 1984, accepté le 5

mars

1985)

Résumé.

2014

L’évolution d’un spectre d’ondes de plasma légèrement instables en présence d’un faisceau élargi

en

vitesse est traitée habituellement par la théorie quasi linéaire. Cependant des simulations numériques et des expé-

riences de laboratoire ont révélé des écarts à la description quasi linéaire dans la présence de structures persistantes

dans l’espace des phases et dans le comportement individuel des modes. On montre dans cet article que l’évolution inattendue des modes individuels peut être expliquée à l’aide d’une interaction des ondes par l’intermédiaire de

perturbations balistiques de grande longueur d’onde. Le point de départ est

une

théorie faiblement non linéaire qui comprend les parties balistiques des perturbations. On établit d’abord

un

système d’équations de base qui

foumit une généralisation de la théorie quasi linéaire. En simplifiant le modèle théorique on arrive à un système d’équations différentielles ordinaires qui sont résolues numériquement dans des cas représentatifs.

Abstract

2014

The evolution of

a

spectrum of weakly unstable plasma waves in the presence of

a warm

beam is

usually treated by quasilinear theory. Numerical simulations and laboratory experiments, however, showed depar-

tures from the quasilinear description both in the presence of persistent structures in phase space and in the beha- viour of individual modes. It is shown in this paper that the unexpected evolution of individual modes can be

explained in terms of interaction of the waves via long

wave

length free streaming perturbations. The starting point

is

a

weakly

non

linear theory in which the free streaming portions of the perturbations are included. A basic system of equations is first derived which provides

a

generalization of quasilinear theory. The theoretical model is further

simplified and leads to

a

system of ordinary differential equations, which

are

solved numerically in representative

cases.

Classification Physics Abstracts

52. 35M

1. Introduction.

The weak warm-beam instability in a one-dimensional electron plasma has been the subject of extensive

theoretical, experimental and numerical work. Early

numerical simulations [1] already revealed departures

from the predictions of quasilinear theory [2], which

were confirmed by experimental studies [3] and by

recent numerical work [4]. The observations were

formulated and interpreted in several languages, but mainly in terms of unexpected field and particle-

motion correlations. The presence of ordered struc- tures in phase space and of convective streams of

particles was noted [5] and compared with a theory

of moderate turbulence (see Refs. [3] and [4] and

references therein). It was also observed and report-

ed [4, 6] that single modes do not in general show a

smooth quasilinear behaviour but that they happen

to rise and decay rather abruptly. The average evolu-

tion of a group of neighbouring modes was found, however, to evolve much more regularly [6].

This body of numerical and experimental data has

lead to extensive theoretical work aimed at revising

and improving quasilinear theory. A thorough review

and a rigorous reformulation of quasilinear theory [7]

showed the importance of mode coupling and gave

a comprehensive statistical description of the evolu- tion of the spectrum of excited waves. An alternative

approach is considered in this paper, which is not sta- tistical in nature. The starting point is a weakly non

linear theory [8, 9], which applies to the evolution of small amplitude plasma waves and whose validity is

limited to a time scale of the order of the bouncing period of trapped particles in the field of the waves

considered. According to this theory, the non linear

evolution of the plasma is described in terms of wave amplitudes and free streaming perturbations. Non

linear interaction of free streaming perturbations with plasma waves, once observed as the « linear side band

effect » [11], has recently been demonstrated numeri-

cally and analytically [12]. In the present work, inter- action of neighbouring modes is found to occur via a

Article published online by EDP Sciences and available at http://dx.doi.org/10.1051/jphys:019850046070112300

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long wave length free streaming perturbation, which

is created by the beating of the modes and interacti with them. This effect is reminiscent of non lineaj Landau damping, but it is distinct from it in two ways the interaction is due entirely to resonant particles anc

the important part is played by the free streaming por- tion of the beat disturbance rather than by its electric field. Non linear mode coupling was considered long

ago in the frame work of weakly non linear theories

[10], but the free streaming portions were consistently neglected, thus missing the main effect.

The physical situation chosen in this paper is the

same as in reference [4]. A one dimensional electron

plasma of length L

=

1 024 À.D is considered and

periodic boundary conditions are applied. The ions

are replaced by a uniform neutralizing background.

The unperturbed distribution function fo(v) has the

form of a main Maxwellian plus a warm beam :

The values of the parameters are also the same as in reference [4] namely :

In numerical simulations, the unstable waves are most conveniently allowed to grow out of a small-

intensity initial noise, whereas in this paper initial

amplitudes of waves will be given values correspond- ing to the onset of non linear effects. The values of the reduced amplitudes :

(where Ek’ is the wave electric field and no the unper- turbed density) will lie between 10- 3 and 10- 2 and

quasilinear evolution will take place for values of

wp t of a few hundred

The paper is organized as follows. In section 2 a

basic system of equations is derived, which is an

extension of the usual quasilinear system of equations

in that it involves the free streaming perturbations of

small wave numbers in addition to the wave ampli-

tudes and to the space averaged distribution function.

In section 3 this system of equations is reduced to a system of ordinary differential equations on the wave amplitudes, the values of the space averaged distri-

bution function and the values of the free streaming perturbations taken for the phase velocities of the

waves. In section 4 the system of equations is modified

by applying a smoothing procedure to the velocity dependence in analogy to a successful practice in

numerical simulations [4]. The equation of the model

are integrated numerically and the results are pre- sented and discussed in section 5.

2. Basic equations,

Let us briefly recall the results of the weakly non linear theory [8, 9] which is the starting point of this work.

A one dimensional electron plasma with period L in

space is considered and the distribution function

f(x, v, t) is expanded in a Fourier series in x in the usual way. In order to treat the non linear interaction of plasma waves, it is convenient to be able to extract from each Fourier coefficient fk(v, t) the portion cor- responding to plasma waves. This is possible in a way which is suggested by the behaviour of fk(v, t) in the

linear theory of plasma waves, namely by its asymp- totic form for large t :

where A:, w: and uk denote the amplitude, frequency

and phase velocity of the wave of wave number k cor- responding to root number a of the dispersion rela-

tion. Ak and Pk(v) are independent of t and are easily expressed in terms of fk(v, 0). The full solution fk(v, t)

of the linearized equation involves an additional rapidly damped term which can also be expressed in

terms of Pk(v). More generally one can establish a correspondence between on the one hand any suffi-

ciently regular function fk(v) and on the other hand a

set of amplitudes a: and a function t/Jk(V) defined in

such a way that they have the above simple time depen-

dence when computed from the solution fk(v, t) in

the linear approximation. This correspondence can

then be used to make a change of unknown functions and translate the Vlasov equation in terms of ak(t) and t/lk(V, t).

The next step in the theory is then to apply an approximation of the Krylov-Bogoliubov type to the system of equations on all, qlk’ Writing

these quantities are of first order in the small para- meter 8 of the theory and, in addition, Ak and Pk are slowly varying functions of t. The small parameter is more precisely of the order of the ratio of the per- turbed plasma density to the equilibrium density and

this turns out to be of the order of kÀ.D Êk or

H 2 where AD is the Debye length, E. the reduced amplitude (wB) of equation (3) and (oB the bounce frequency

of the trapped electrons in the wave potential. The

amplitude Ak is related to the wave potential 0’ and

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The final equations of the weakly non linear theory

are equations (44.14) and (4.15) of reference [9] or equations (33) and (46) of reference [8]. A detailed analysis of their derivation shows that they are valid

over a time scale of the order of 1/((opl/1-C-) provided

contributions to Ak and t/Jk of order larger than one in

s are neglected. Additional approximations will now

be made in order to simplify these equations for the problem considered in this paper.

Let us first consider equation (4.15) of reference [9]

which describes the creation of a free streaming per- turbation t/Jk(V, t) through the interaction of a wave of

amplitude ak, with another wave of amplitude ak" or

with a free streaming perturbation t/1k"(V, t). This equation contains « secular terms » growing propor- tional to t, which arise in the differentiation of 41k "(v, t)

with respect to v, when it is written in the form of

equation (4). The approximations to be made will consist essentially in neglecting terms which are small compared to the secular terms. In so doing, it is most important to make sure that the neglected terms are

not singular for the values of the velocity considered,

in particular for the phase velocity u" of the k" wave.

To this end one can write equation (4.15) of refe-

rence [9] in the following form by discarding terms

that are both regular as functions of the velocity and

non secular in their time dependence :

where q and q" are the signs of k and k" and where the function Gk,,(v, t) is regular in v and slowly varying in

time. It is seen that the term containing Gk" is less secular than the remaining part of the expression in square brackets at least if v is close to u". Thus if a group of neighbouring waves is excited and if v lies in the range of their phase velocities, the contribution of Gk" may be neglected. Further the values of k considered are small since

they are the differences of neighbouring wave numbers, and for small values of k, e* (k, v) are equal to a good approximation so that the factors 8" and En" may be dropped Writing the equation in terms of the slowly varying quantities Ak and Pk, we obtain the first basic set of equations :

with

and where co’ t and w" t have been written for brevity instead of the time integrals of w’(t) and w"(t).

The second set of equations, i.e., equation (4.14) of reference [9], gives the evolution of the wave amplitudes

under the influence of the free streaming perturbations. Neglecting the mode coupling terms, which are far from .resonant, this set of equations reduces to :

with

where Ck is the usual Landau path of integration.

The system of equations must now be completed by adding the equation for the space averaged distri-

bution function fo(v, t). This equation can be simplified

in the same way as the equation for the free streaming perturbation by keeping only the most secular terms

with a result similar to (7) :

where u stands for ulk’ and where values of P, y corres-

ponding to phase velocities Uk and uk of the same sign

should be retained.

The basic equations (7), (8), (10) apply to the situa-

tion considered where a spectrum of weakly unstable

waves is excited. This system of equations appears as

an extension of the classical quasilinear theory, in that

the time evolution of the wave amplitudes interacts

not only with the space averaged distribution function, but also with free streaming perturbations of long

wave length. The time scale over which this descrip-

tion is valid is essentially that of the underlying weakly

non linear theory, namely the bouncing period of

trapped electrons in a representative wave.

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3. System of ordinary differential equations.

The basic equations can be further simplified by conti- nuing to select the most secular terms. Provided fo(v)

is not too small, the following approximation can be

made in equation (7) :

Then equation (7) is no longer differential in v,

which now enters merely as a parameter. As the deriva- tive ð/ðvPk is needed in equation (8), one is lead to

differentiate equation (7) with respect to v and to make the additional approximation :

Approximations of the same type can be made on equation (10) and on this equation differentiated with respect to v. Thus a complete system of equations is

obtained in which v enters as a parameter. According

to equation (8) the only relevant values of v are the

phase velocities of the excited waves, which we will consider to be a finite number corresponding to the

case of a plasma of finite length L.

The wave numbers are then multiples of k1 = 2 n/L

and the index k can be conveniently replaced by the integer n

=

k/k1. According to the chosen form (1) of fo(v), the excited waves correspond to positive phase

velocities and to a certain interval of I n I

The index, a, fl or y on the wave amplitudes and phase

velocities will be dropped with the understanding that only waves of positive phase velocities are considered

(then A-n

=

(An)*). The free streaming perturbations

are created with wave numbers ± mk1 with 1 , m

N2 - N1 and it is easily seen that only the P_ m enter equation (8). The outcome of the approximations is

then a system of ordinary differential equations on the following unknown functions of the time :

A few additional simplifications can be made to this

system of equations. First, if N2 - N1 N l’ it is a

consequence of the equations that :

and equation (8) can be simplified accordingly. Further

in differentiating equation (7) with respect to v, the

term involving 010v eikUt may be neglected.

Finally the following system of equations is obtain-

ed :

Finally the following system of equations is obtained :

t

with and the notations :

The frequencies and the phase velocities Cok and u,,, are given by the roots of the dispersion relation and have

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small imaginary parts :

In order to get a closed system of equations most simply, one can take Yn(t) proportional to fo(un, t) :

where Yn(O) is the linear growth rate corresponding to expression (1) for

It was assumed from the start that only free streaming perturbations of small » wave numbers came into

play, which is the case if the spectrum of excited waves is fairly narrow so that N2 - N 1 N 1. This was used in simplifying equation (6) and again in simplifying equation (9) according to equation (14). This assumption is fairly well justified in the examples to be discribed in section 5, but not really in the case of the numerical simula- tion of reference [4], where the full spectrum of unstable waves is excited from the initial distribution function (1).

The system of equations (15-17, 22) is still meaningfull in the case of a single wave, when it reduces to a single equation on fo(un, t)

According to this equation, fo(un, t) would drop to zero very suddenly after a time of the order of OJB 1, denoting by COB the angular bounce frequency of the trapped electrons defined by equation (5). It should be noted, however,

that the approximations leading to equation (23) are no longer valid once fo(un, t) has become too small. The

same remark applies to equation (15-17) whenever one of the quantities fo’(u,,, t) tends to zero.

The case of two waves is also interesting. If n and n + 1 are the two wave numbers considered, equation (15)

and (16) can be brought back to a second order differential equation on An(t), which takes the following simple

form after some additional approximations :

A formal asymptotic expansion of the solution for large t shows that An(t) is likely to behave like :

with

which means that the relevant time scale for non linear interaction of the two waves is roughly WB 1.

4. Smoothing procedure.

In some numerical simulations it was found useful

to use a smoothing procedure in order to avoid too sharp dependences on the velocity leading to numerical

difficulties [4]. Typically the velocity distribution at every point in space would be smoothed over a small

velocity interval w (a small fraction of the thermal

velocity) after every time interval At. The smoothing procedure would be for instance :

and the results would prove insensitive to the values of w and At within a suitable range of values.

It was thought interesting to try and introduce an

analogous smoothing procedure in the analytical theory to make the comparison with numerical work

more realistic. In addition one may hope that a reaso-

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nable smoothing procedure can suppress numerical difficulties in the solution of the differential equations

of section 3 without modifying the results substan-

tially. Such difficulties could probably be avoided by purely numerical methods in the code that solves the differential equations. But it was considered preferable

to incorporate a smoothing procedure in the analy-

tical theory so as to display its significance more clearly.

If there is any need to smooth the velocity depen- dence, it certainly arises in expressions of the form :

that occur in the right hand side of equations (7) and (10) for Pk and fo, with k", u" for k, u. These expressions

are portions of the solution of the linearized Vlasov

equation for wave number k" and we will interpret fo(v) Hk(v, t) as the solution of the equation :

that vanishes for t

=

0 and we will examine the effect of a smoothing procedure of the form (27) on this

solution.

It is shown in Appendix A that this effect can be

simulated, at least semi quantitatively, by adding a

small diffusion term to equation (29) :

provided Av and At satisfy

An approximate solution of equation (30) can be

found for times limited by

and this is done in Appendix B. This solution is :

The analogue of the smoothing procedure will therefore consist in modifying the functions Hn(v, t)

and Hn(v, t) defined by equations (19) and (20) in the following way :

5. Numerical results.

The system of equations defined in sections 3 and 4 was

integrated numerically for various values of the para- meters. In the absence of smoothing the equations

derived in section 3 can be integrated with standard

codes. Still the computation is usually stopped by

numerical difficulties which apparently cannot be

overcome by simply reducing the time step. But as will be seen below, whenever this happens the system of equations appears no longer to be valid

The unperturbed distribution function fo(v) was

chosen to have the form of equation (1) with the values of the parameters given by equation (2).

The initial amplitudes of the waves were given such

values that the interesting effects would occur on a

time scale for which the theoretical model is valid.

As was mentioned previously, this time scale is of the order of the bouncing period 2 Tr/cos of the trapped

electrons in the waves considered. A suitable range of values of the reduced amplitudes defined by equa- tion (3) then turns out to be between 10-3 and 10 - 2.

The calculations presented in the following were made with £

=

3 x 10-3 for all waves at t

=

0, so that

2 a/COB 260 cop 1. With these initial amplitudes the

effects of non linear interaction are clearly observed

for wp t 100, as well as the evolution of the growth

rate.

The choice of the smoothing parameter, i.e., the

diffusion coefficient D in velocity space used in equa- tions (35, 36), was also inspired by the numerical

simulation of reference [4] and most of the calculations

were made for :

The values of D chosen in each particular case will

be defined with reference to this standard value.

5.1 THE TWO-WAVE PROBLEM.

-

In the case of two waves of wave numbers nk1 and (n + 1) k1, the only significant initial value is that of I Ên+ 1 I. The results

are shown in figure 1 for a representative’case : n

=

30,

Ên +1

=

3 x 10-3. The solid curves give the evolution of E30(t) and E31(t) as obtained without smoothing procedure. The computing was stopped at wp t

=

55

because the values of fo(un+ 1, t) was becoming too

small for the equations to remain valid. The dashed lines correspond to the calculation with standard

smoothing, in which case the computing was stopped

for the same reason at wp t

=

75. The behaviour observed with and without smoothing is qualitatively

the same, although the difference is not negligible. The

decrease in amplitude of the n

=

30 wave is clearly

seen and shows the importance of the type of interac- tion described by the system of equation of section 3.

This effect will become dramatic in cases with more

than two waves.

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Fig. 1.

-

Case of two

waves

of

wave

numbers 30 k

1

and

31 k18 The reduced amplitudes (defined by Eq. (3)) P3, and E31

are

plotted versus t for initial values 3 x10-3 . The solid

curves show the results without smoothing and the dashed

curves

correspond to standard smoothing.

5.2 THE FOUR-WAVE PROBLEM.

-

With four waves

the situation is much more complicated since free streaming perturbations are created with three wave

numbers k1, 2 kl, 3 k, and since the results depend sharply on the initial phases of the waves. The calcula- tions were made for four waves lying in the middle of the unstable spectrum with n

=

30 to 33. The 33

wave is not affected by the free streaming perturbations

and the 30 wave on the contrary feels the action of the three wave numbers k1, 2 k1, 3 k1. In order to see the

relative importance of the free streaming perturbations

of the three wave numbers calculations were made by truncating the sum over m in equation (15) to m M with M

=

1, 2, 3. The results are shown in figure 2

for a representative case with equal initial amplitudes

and phases of the four waves and with the standard

smoothing. The solid curves correspond to M

=

3, i.e., to no truncation. For the 32 wave the M = 2 and M

=

1 curves are not shown : in fact they are

very close to the M

=

3 curve shown, as one would expect since the 32 wave feels only the effect of the k1

free streaming perturbation. For the 31 wave the two

curves M

=

2 and M

=

3 almost coincide (only the

M

=

3 curve is shown), but the M

=

1 curve (dotted line) is markedly different, which means that the 2 ki

free streaming perturbation has a large effect on the

31 wave. For the 30 wave the three curves M

=

1, 2, 3

are shown and the difference between M = 2 and

Fig. 2.

-

Case of 4 waves of wave numbers 30 ki to 33 kl*

The reduced amplitudes t

are

plotted

versus

t for initial values of 3

x

10-3 and equal initial phases. Standard smoothing is used Free streaming perturbations of

wave

numbers mkl (I m M)

are

included. Dotted, dashed

and solid curves correspond respectively to M

=

1, 2, 3.

M

=

3 is much less marked than between M

=

1 and M

=

2. Thus the effect of the 2 ki wave number on the

30 wave is large and the 3 ki wave number is less

important. A note-worthy feature of figure 2 is also the fact that all curves have a decreasing portion, starting

at Mp t N 30, so that the total energy of the waves decreases significantly before starting again to increase sharply.

A striking fact in the case of more than two waves

is the sharp dependence of the evolution of the waves

on their initial phases. Typical results are shown in figure 3 for the same excited waves and initial ampli-

tudes as in figure 2, but with two different sets of phases.

Note in particular the very different behaviour of the 30 wave in figure 2 (solid curve) and in figure 3 (dashed curve). Still another set of phases is used in figure 4

with the same initial amplitudes and the Ego curve is

seen to exibit a remarkable dip.

All curves shown in figures 2 and 3 were computed

with the standard smoothing. In order to appreciate

the effect of smoothing, results are shown in figure 4 for

the same initial data and with standard smoothing (solid curves), half standard smoothing (dashed curves)

and no smoothing (dotted curves). In the latter case the

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Fig. 3.

-

Four waves with the same

wave

numbers and

initial amplitudes

as

in figure 2. Solid curves correspond

to the phases (0, 0, n, n) and the dashed curves to the phases

computation was carried only up to cop t

=

55 on

account of too small values of fo(un). A fast decrease of fo(un) may be spurious and may be due to the break down of the approximations made in section 3, so that the results obtained with a certain degree of smooth- ing may be more representative of the solution of the

more exact equations of section 2. In order to docu-

ment this point, the evolution of fo(un) is shown in

figure 5 for n

=

30 and 31 with the same parameters as in figure 4 and with the same meaning of solid, dashed

and dotted curves. The decrease is clearly faster

without smoothing, but the curves with standard and half standard smoothing are similar. The curve

n

=

31 with half standard smoothing was carried through up to wp t

=

100 regardless of the excessively

small values of fo(un). It can be inferred from these results that the smoothing procedure, although it has a

non negligible effect, probably leads to qualitatively

correct results beyond the range of validity of the equations without smoothing.

5.3 THE MANY-WAVE PROBLEM.

-

A comprehensive description of what happens with a large number

of waves is impossible to give. But there remains the

Fig. 4.

-

Four waves with the same wave numbers and initial amplitudes as in figure 2 and with phases 0, 0, n/2 ’ 2 ’

Results with different values of the smoothing parameter

are shown : standard smoothing (solid curves), half standard (dashed curves) and no smoothing (dotted curves).

Fig. 5.

-

Four waves with the same values of parameters

as in figure 4. The evolution of fo(un) is shown for n

=

30

and 31 and for the same values of the smoothing parameter

as in figure 4 : standard (solid curves), half standard (dashed curves) and no smoothing (dotted curves).

general fact that very different behaviours of the waves can be observed by changing only their initial phases.

As was done in numerical simulations [4] the possible

evolutions can be explored by starting with randomly

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chosen initial phases. A number of runs were made

with 8 waves and it appeared that anomalous beha- viour of a wave, i.e., a sharp dip in the Ên(t) curve, was

less frequent than with 4 waves. A definite case of such

behaviour is shown in figure 6, where the curves P.(t)

are shown for n

=

28 and 29 out of a set of 8 waves,

n

=

26 to 33. This figure can be compared with a typical result of numerical simulation (Ref. 4, Fig. 2)

and the behaviour of the two neighbouring waves is

seen to be strikingly similar. It should be mentioned

that the curves of figure 6 (solid lines) were obtained

with a fairly strong smoothing of four times the stan- dard. The dashed curves show the results with twice the standard smoothing, in which case the computa- tion could not be carried beyond wp t

=

60. In most

cases with 8 waves, without any markedly anomalous

behaviour of individual waves, no numerical diffi- culties were encountered with twice the standard

smoothing.

An attempt was also made at testing a statistical

prediction of reference [7] by running a series of 8-wave

cases with randomly chosen phases. The observed

growth rate of each wave yexp is predicted to be greater than the quasilinear growth rate ykl by a certain

factor provided suitable average values are taken for these growth rates. For yzxP the following weighted

Fig. 6.

-

The evolution of two waves is shown out of

a

set of 8

waves

(n

=

26 to 33). The solid curves correspond to

4 times the standard smoothing and the dashed curves to twice the standard smoothing.

average is considered :

the sum extending over the M cases computed. The quasilinear growth rate is defined from the instanta-

neous space averaged distribution function fo(v, t)

also averaged over the M cases, which amounts to

taking the arithmetic mean of the M values of ykl(t)

for each k and t. Then the ratio yexp/yq’ should have a

definite value greater than one, which is estimated to be 2.2 in reference [13]. The validity of this result is

subject to two inequalities being satisfied, the first

of which is characteristic of a regime where quasilinear theory is invalidated by additional non linear effects [13, 14].

where Dkl is the quasilinear diffusion coefficient in

velocity space Dkl(v) taken for v

=

úJk/k. The second inequality means that the waves are weakly dispersive

and it can be written approximately [7,13,14] :

The values of QD, Yk and vd;sp are shown in table I for a

representative wave (n

=

29) and several values of the time. It is seen that the double inequality is marginally

satisfied in the middle of the time range considered,

so that a qualitative test may be meaningful.

A series of 30 cases of 8 waves (n

=

26 to 33) were

run with randomly chosen phases. The other para- meters were the same as for the cases considered pre-

viously and a smoothing of twice the standard value

was used. In three cases out of 30 the calculation was

stopped half way to the maximum time of 120 cop

and in three other cases it was stopped between

100 w; 1 and 120 w; 1. The results on the growth rates

are shown in figures 7, 8, 9 for a few waves in the middle

Table I.

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Fig. 7.

-

Time evolution of the quasilinear growth rate averaged

over a

series of 30 cases of 8 waves with randomly

chosen phases.

Fig. 8.

-

Time evolution of the

«

experimental

»

average growth rate computed according to equation (38) from the

same cases

as

in figure 7.

Fig. 9.

-

Ratio of the average growth rates shown in figures 7 and 8.

of the spectrum. First in figure 7 ykl is seen to decrease gently as one would expect from quasilinear theory,

but not quite monotonously. The behaviour of yexp appears, however, much more complicated in figure 8. The ratio y"PI-)Ak’ is shown is figure 9 and it

does take values roughly equal to those predicted

for times greater than about 60 wp-1.

Acknowledgments.

The hospitality of the Centre de Physique Th6orique

de 1’Ecole Polytechnique during the course of this

work is gratefully acknowledged. The author also whishes to thank G. Laval and D. Pesme for stimulat-

ing discussions.

Appendix A

Let the smoothing operation on the function g(v, t) be performed at regular time intervals t1+ 1 - ti

=

At and

assume this operation to take the form :

(12)

with

Then the procedure is the following when applied to the solution of equation (29) for g(v, t) :

If F(v) is a regular function of v which varies little over Av :

with

Thus :

and if ei’v " and fo(v) vary more slowly than g with v :

Now putting

and assuming that terms of order D(At)2 may be neglected, we get :

which is an approximate step by step solution of :

If W denotes the interval over which g varies appreciably with v, the conditions of validity of (A. 5) are :

Appendix B.

The solution of equation (30) for g(v, t) can be found by means of a Fourier transformation on v :

The transformed equation is :

(13)

and it can be solved by using u

=

y + kt as a new variable. The solution that vanishes for t

=

0 is :

The solution for g is obtained as the inverse transform and can be written :

with

It turns out that K(v, t, s) can be easily computed if fo(v) is a Maxwellian :

and the result is :

with

It is seen that for

the expression for K(v, t, s) simplifies considerably and reduces to its value for D

=

0 :

so that the solution for g(v, t) is :

In fact this approximate solution for g is valid for more general functions fo(v) subject to condition (B. 5).

The same type of calculation can be made if fo(v) is for instance the nth derivative of a Maxwellian, still leading

to expression (B. 6) for g. Thus the approximate solution (B. 6) for g is valid when fo (v) is any linear combination

of Maxwellian functions multiplied by polynomials of v.

(14)

References

[1] DAWSON, J. and SHANNY, R., Phys. Fluids 11 (1968)

1506.

MORSE, R. and NIELSON, C., Phys. Fluids 12 (1969) 2418.

[2] DRUMMOND, W. E. and PINES, D., Ann. Phys. (N.Y.)

28 (1964) 478.

VEDENOV, A. A., VELIKHOV, E. D. and SAGDEEV, R. Z., Nucl. Fusion Suppl. 2 (1962) 465 and 1 (1961) 82.

[3] KRIVORUCHKO, S. M., BASHKO, V. A. and BAKAI, A. S.,

Sov. Phys. JETP 53 (1981) 292.

[4] ADAM, J. C., LAVAL, G. and PESME, D., Proc. Intern.

Conf.

on

Plasma Physics, Nagoya (1980), Vol. II,

10 B 3, p. 298.

[5] BAKAI, A. S. and SIGOV, Yu. S., Sov. Phys. Dokl. 22 (1977) 734.

[6] BISKAMP, D. and WELTER, H., Nuclear Fusion 12

(1972) 89.

[7] ADAM, J. C., LAVAL, G. and PESME, D., Ann. Phys.

Fr. 6 (1981) 319.

[8] TROCHERIS, M., Plasma Phys. 21 (1979) 75.

[9] TROCHERIS, M., J. Math. Phys. 21 (1980) 941.

[10] ERIEMAN, E., BODNER, S. and RUTHERFORD, P., Phys.

Fluids 6 (1963) 1298.

ERIEMAN, E. and RUTHERFORD, P., Ann. Phys. (N. Y.) 28 (1964) 134.

[11] MORALES, G. J. and MALMBERG, J. H., Phys. Fluids

17 (1974) 609.

[12] ADAM, J. C. and TROCHERIS, M., Phys. Fluids 27 (1984) 600.

[13] LAVAL, G. and PESME, D., Phys. Rev. Lett. 53 (1984)

270.

[14] LAVAL, G. and PESME, D., Phys. Fluids 26 (1983) 52.

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